View from above orbital plane
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View from above satellite
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Ground track
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The orbit data is extracted from the following two-line orbital elements,
1 13992U 83031B 24284.35547951 .00001249 00000-0 42962-3 0 9990
2 13992 74.0516 144.2520 0005424 191.7566 168.3462 14.37051247172179
| Epoch (UTC): | 10 October 2024 08:31:53 |
| Eccentricity: | 0.0005424 |
| inclination: | 74.0516° |
| perigee height: | 764 km |
| apogee height: | 772 km |
| right ascension of ascending node: | 144.2520° |
| argument of perigee: | 191.7566° |
| revolutions per day: | 14.37051247 |
| mean anomaly at epoch: | 168.3462° |
| orbit number at epoch: | 17217 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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